Gas Turbine Single Annular Combustor Sector Aerodynamics

Author:

Mohammad Bassam1,Cai Jun1,Jeng San-Mou1

Affiliation:

1. University of Cincinnati

Publisher

American Institute of Aeronautics and Astronautics

Reference37 articles.

1. 1Beer,J.M.,andChigier,N.,Combustionaerodynamics,AppliedSciencePublishersLTD,London,1972.

2. 2Gupta,A.K.,Lilley,D.G.,andSyred,N.,Swirlflows,AbacusPress,1984.

3. Combustion in swirling flows: A review

4. A study of a bluff-body combustor using laser sheet lighting

5. Phase averaging of the precessing vortex core in a swirl burner under piloted and premixed combustion conditions

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1. Design of an optically accessible single cup sector of a full-scale annular gas turbine combustor;AIAA SCITECH 2023 Forum;2023-01-19

2. Effect of primary hole parameters on combustor performance within a slinger combustor;Applied Thermal Engineering;2022-11

3. Gas Turbine Single Annular Combustor Sector: Combustion Dynamics;48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition;2010-01-04

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